M362713 八、新型說明： 【新型所屬之技術領域】 本創作係有關於一種「四旋翼無人飛行载具結構」， 其係於一基座及一罩體間容設一控制電路以驅動四傳動 裝置之馬達，該傳動裝置係環設於罩體外侧且各組設有翼 片而形成一四旋翼無人飛行載具’而可利用馬達之轉速及 差速來控制每一旋翼’使該飛行載具可順利翱翔於空中並 於空中進行轉向、前進或定點旋轉。 【先前技術】 隨著科技的進步’人類對於大型飛機發展之技術已日 趨成熟，於是便有許多學者轉向於微型無人載具飛機之發 展，而其中最讓人感興趣的即是微飛行器（微飛機）及近年 來新興之熱門機種無人載具，微飛機與無人載具之所以讓 人感興趣的地方即是它在軍事上的用途包含有偵查、突襲 等’更可應用於搜山.尋人等多種任務而極具研究價值， 然，目前研發之無人飛機大多以直升機（如台灣公告第 M333220、M333222、M332509)式的結構設計為主，以致飛 行上及空中旋轉繞行上仍然受機尾的影響而須精確掌控 飛行空間方能順利操控，令使用上較為受限不便。 本創作人有鑑於上述習式之缺失，乃思及創作的意 念，經多方探討並試作樣品試驗，及多次修正改良，乃推 出本創作者。 【新型内容】 本創作之主要目的，乃在提供一種四旋翼無人飛行载 具結構’其係於—基座及—罩體間容設〆控制電路以驅動 M362713 四傳動裝置之馬達，該傳動裝置係環設於罩體外侧且各組 設有翼片而形成一四旋翼無人飛行載具’而可利用馬達之 轉速及差速來控制每一旋翼，使該飛行載具可順利翱翔於 空中並於空中進行轉向、前進或定點旋轉。 【實施方式】 餘下茲配合圖式，詳細說明本創作之最佳實施例如 . 后： 如第一圖所示係為本創作之立體圖（請同時參考第 一、二圖），其係包含：一基座（10)、一控制電路（20)、 * 一罩體（30)及四傳動裝置（40)，其中基座（10)之頂面凹設 一平台（U)，底面凹設一較大之第一槽部（12)及一較小之 第二槽部（13)呈矩形狀相鄰，平台（11)之兩側對稱貫設一 呈彎弧狀之通口（14)與第一槽部（12)相通以供控制電路 (20)之線路（A)繞設’且中心貫設一與第一槽部（12)相通 之透孔（15)，並於第二槽部（13)之頂面貫設一限位孔 (16) ’於平台（11)之底面順第一槽部（12)之兩外侧對稱凸 設有若干片狀往下漸擴之撐腳（17)，控制電路（20，請同 鲁 時參考第四圖）係設一為鋰聚充電電池之供電器（21)與一 具控制開關（221)之無線接收器（22)、三可偵測角迷度之 感應器（23，可為陀螺儀）、二混控器（24)及四速控器（25) 相配合以獨立控制四傳動裝置（40)之作動，並設一為無線 發射器之遙控器（圖式未予以繪出）以發射指令至無線接 受器（22)而形成一控制迴路，該遙控器係具有油門控制、 方向舵控制、升降舵控制及副翼控制以傳達指令至控制電 路（20)使四傳動裝置（40)得以接收命令，並利用四傳動裝 M362713 置（40)之轉速及差速來操控該飛行載具在空中的轉向、前 進或定點旋轉，其中供電器（21)係容設於第一槽部（12) 内，接收器（22)及三感應器（23)係置設於平台（11)上，並 設一板狀固定座（26)供四速控器（25)置設定位，且固定座 (26)之中心設一透孔（261)，控制開關（221)係容設於第二 槽部（13)内且頂面設有切換鍵（2211)恰容嵌定位於限位 孔（16)，罩體（30,請同時參考第五圖）之底面凹設一與平 台（11)相配合之容納槽（31)，外圍環狀凸設四套接管（32) 與容納槽（31)相通，並於容納槽（31)之頂面中心向下凸設 • 一具内螺孔（331)之頂柱（33)穿設於固定座（26)之透孔 (261)與平台（11)之透孔（15)相對以供一為螺絲之組件 (34)鎖設固定’令控制電路（2〇)恰隱藏於平台（11)及容納 槽（31)間，於每一套接管（32)之内部各套設一管狀撐桿 (35，請同時參考第六、七圖），於撐桿（35)之末端設一貫 穿於上下兩侧之定位孔（351)與一套接座（36)相配合，於 套接座（36)之一側設一套管（361)與撐桿（35)相套設且設 一與疋位孔（351)相對之套孔（362)供一支柱（363)穿設固 ♦ 定，另一側設一呈管狀之容置區（364)以供傳動裝置（40) 組没，該容置區（364)係與套管（361)設呈相通，令控制電 2(20)之線路(^)可由容納槽（31)内部延套接管（32)及撐 |于（35)穿繞至容置區（364)與傳動裝置（4〇)相接通，於套 s (361)—侧杈向開設一與内部相通之彈性束孔（加5)，並 於彈性束孔（365)之兩侧對稱設—具穿孔⑽）之夾片 (36:)供一為螺絲及螺帽之組件(368)鎖設，使夾片（367) f彈性束孔（365)可藉由組件（368)之鎖迫產生相對的夾 力促使套管（361)與撐桿（35)之組合更為穩固而不虞 M362713 鬆動，並於每一撐桿（35)之底端各設一與罩體（go)相頂抵 - 之支桿（352)，且設一為尼龍線之撓性元件（3631)以等距 離同步繞設固定於每一支柱（363)，令撐桿（35)得以受支 桿（352)及撓性元件（3631)之牽制達到補強之目的而不虞 文外力之影響，於罩體（30)之頂面縱向貫設若干與套接管 (32)相通之螺孔（301)供一螺絲（3〇2)鎖設恰迫抵於撐桿 (35)之表面，且撐桿（35)亦可設一通孔（353)與螺孔（3〇1) 相對而同步受螺絲（302)之牽制定位，容置區（364)之一側 一體向外對稱凸設一撐片（369)而形成一夾置空間 春（3691)，傳動裝置（4G)係設-為馬達（41)之動力源恰容套 固定於容置區（364)及夾置空間（3691)，該馬達（41)係設 一較小控之齒狀主動輪（411)與一較大徑之齒狀被動輪 (412)相嚙合而形成一減速齒輪馬達，於被動輪（412)之中 心凸設一具外螺紋段（421)之作動桿（42)，並設一中心呈 套孔⑽）之連結件（43)穿套於作動桿（42)，使作動桿（42) 突伸於套孔（431)外，於套孔（431)之底端設-内螺紋段 (432’可於内部埋設一螺帽）恰與外螺紋段（421)相鎖結固 鲁定，倾-墊片（44)及-螺帽（44,）依序穿設於作動桿 (42)而鎖迫於連結件（43)之頂面’於連結件⑽之兩側對 [體延設-具若干穿孔(433)之組接片(434)各與一為 混合型且具若干穿孔（4⑴之翼片（45，屬於内凹翼）鎖固 而形成四旋翼（如第八圖所示），該四旋翼於每—撲桿⑽ 上呈兩兩-組相對設置且為不同轉向之兩個正旋翼（ 及兩個逆旋翼（453)。 其欲飛行時（如第九圖所示），係先將控制開關（221) 之切換鍵（22⑴切換於⑽，使控制電路⑽及每一傳動 M362713 裝置（40)與供電器（21)導通得以保持供電狀態，當接收器 (22)收到遙控器（如油門、方向舵、升降舵及副翼）所發射 之訊號，接收器（22)即會把訊號（即電流量大小）傳遞給速 控器（25)，速控器（25)即會依訊號（即電流量大小）獨立驅 動每一傳動裝置（40)之馬達（41)，令主動輪（411)得以帶 動被動輪（412)、作動桿（42)、連結件（43)及翼片（45)同 步旋動’並以馬達（41)之轉速及差速來控制正旋翼（452) 及逆旋翼（453) ’使該飛行載具可順利翱翔於空中並於空 中進行轉向、前進或定點旋轉，同時，利用速控器（25) • 前的混控器（24)以控制四旋翼（即正旋翼452與逆旋翼 453)在空中的轉向，且當飛行載具於空中飛行及轉向時， 利用感應器（23)介於接收器（22)與混控器（24)間而具備 偵測角速度之功能即可平衡每一馬達（41)之差速，俾可避 免相對之馬達（41)差速過多以保持該飛行載具於空中飛 行及轉向之平穩，進而降低空中的失事率。 綜上所述，本創作確實已經達於突破性之結構，而具 改良之創作内容，同時又能夠達到產業上利用性與進步 • 性’且本創作未見之於任何刊物，亦具新穎性，當符合專 利法第九十三條、第九十四條之規定，爰依法提出新型專 利申請’懇請肖局審查委員授予合法專利權，至為感禱。 唯以上所述者，僅為本創作之一可行實施例而已，當 不能以之限定本創作實施之範圍；即大凡依本創作申請專 利範圍所作之均等變化與修飾，皆應仍屬本創作專利 之範圍内。 M362713 【圖式簡單說明】 第一圖：係為本創作之立體分解圖。 第二圖：係為本創作之基座正面立體放大圖。 第三圖：係為本創作之基座底面立體放大圖。 第四圖：係為本創作之控制電路與基座之立體放大 圖。 第五圖：係為本創作之罩體剖面圖。 第六圖：係為本創作之傳動裝置局部放大組合圖。 第七圖：係為第六圖之立體分解圖。 • 第八圖：係為本創作之立體組合圖。 第九圖：係為本創作之使用狀態圖。 【主要元件符號說明】 10…. ••基座 ll·". "平台 12…. ••第一槽部 13…. ••第二槽部 14···· .·通口 15…. ••透孔 16···· ••限位孔 17···· ••撐腳 20···· ••控制電路 2l··.. ••供電器 22···· ••接收器 221.. …·控制開關 2211· •…·切換鍵 23···· …感應器 24···· ••混控器 25···· …速控器 26···· ••固定座 261" …·透孔 30···· ••罩體 301- …·螺孔 302... …螺絲 31- …容納槽 32…. ••套接管 33- …頂柱 331··· …内螺孔 34… …組件 M362713M362713 VIII. New Description: [New Technology Field] This creation department is about a "four-rotor unmanned aerial vehicle structure", which is equipped with a control circuit between a base and a cover to drive the four transmissions. a motor, the transmission is arranged on the outer side of the cover body and each group is provided with a fin to form a four-rotor unmanned aerial vehicle', and the speed and differential speed of the motor can be used to control each rotor' to make the flight carrier Can fly in the air and make steering, forward or fixed rotation in the air. [Prior Art] With the advancement of technology, 'human technology for the development of large aircraft has matured, so many scholars have turned to the development of micro-unmanned vehicles, and the most interesting one is the micro-aircraft (micro Aircraft) and the emerging hot models of unmanned vehicles in recent years. The reason why micro-aircraft and unmanned vehicles are of interest is that their military uses include investigations, raids, etc. People and other tasks are of great research value. However, most of the unmanned aircraft currently being developed are mainly designed by helicopters (such as Taiwan Announcement No. M333220, M333222, M332509), so that they are still subject to flight and air rotation. The influence of the tail must be precisely controlled by the flight space for smooth operation, which makes the use more limited and inconvenient. In view of the lack of the above-mentioned formulas, the creators of this creator have been explored and tested for sample tests and many revisions and improvements. [New content] The main purpose of this creation is to provide a four-rotor unmanned aerial vehicle structure that is equipped with a control circuit between the base and the cover to drive the motor of the M362713 four-transmission device. The mooring ring is disposed outside the cover body and each group is provided with a fin to form a four-rotor unmanned aerial vehicle', and the rotational speed and differential speed of the motor can be used to control each rotor, so that the flying vehicle can smoothly fly in the air and Steering, advancing or fixed-point rotation in the air. [Embodiment] The following is a detailed description of the best implementation of this creation. For example: As shown in the first figure, it is a perspective view of the creation (please refer to the first and second figures at the same time), which includes: a base (10), a control circuit (20), a cover (30) and a four-transmission device (40), wherein a top surface of the base (10) is recessed with a platform (U), and a bottom surface is recessed The first large groove portion (12) and the smaller second groove portion (13) are adjacent to each other in a rectangular shape, and the two sides of the platform (11) are symmetrically arranged with a curved opening (14) and the first A slot portion (12) communicates with the line (A) of the control circuit (20) around the opening and centrally defines a through hole (15) communicating with the first groove portion (12), and in the second groove portion ( 13) A limiting hole (16) is disposed on the top surface of the platform (11). The bottom surface of the platform (11) is symmetrically convexly disposed on the outer side of the first groove portion (12). The control circuit (20, please refer to the fourth picture with Lu time) is provided with a power supply (21) for the lithium poly charging battery and a wireless receiver (22) with a control switch (221), and three detectable angles. Sensor of the fascination (2 3, can be used for the gyroscope), the second mixer (24) and the four-speed controller (25) to independently control the operation of the four-transmission device (40), and set a remote controller for the wireless transmitter (pattern) Not drawn) to generate a control loop by transmitting a command to the wireless receiver (22) having throttle control, rudder control, elevator control and aileron control to convey commands to the control circuit (20) to enable the four transmissions The device (40) is capable of receiving commands and utilizing the rotational speed and differential speed of the four-drive M362713 (40) to control the steering, forward or fixed-point rotation of the flight vehicle in the air, wherein the power supply (21) is housed in the first In a slot portion (12), the receiver (22) and the three inductors (23) are disposed on the platform (11), and a plate-shaped fixing seat (26) is provided for setting the four-speed controller (25). a hole, and a through hole (261) is disposed in the center of the fixing base (26), the control switch (221) is received in the second groove portion (13) and the top surface is provided with a switching button (2211). The limiting hole (16) and the bottom of the cover (30, please refer to the fifth figure at the same time) are recessed to match the platform (11). The groove (31) has a peripheral ring-shaped protruding four-piece connecting pipe (32) communicating with the receiving groove (31) and protruding downward from the center of the top surface of the receiving groove (31). • A top of the inner screw hole (331) The through hole (261) of the column (33) penetrating the fixing seat (26) is opposite to the through hole (15) of the platform (11) for locking and fixing the assembly (34) of the screw (2) ) is hidden between the platform (11) and the receiving groove (31), and a tubular strut (35, please refer to the sixth and seventh figures at the same time) in each set of the connecting tube (32), in the strut ( 35) The positioning hole (351) penetrating the upper and lower sides is matched with a set of sockets (36), and a sleeve (361) and a strut (35) are arranged on one side of the socket (36). The sleeve is sleeved and provided with a sleeve hole (362) opposite to the clamp hole (351) for a post (363) to be fixedly disposed, and the other side is provided with a tubular receiving portion (364) for transmission The device (40) is not in the group, and the accommodating area (364) is in communication with the sleeve (361), so that the line (^) of the control unit 2 (20) can be extended from the inside of the accommodating groove (31) (32) And the support|(35) is wound to the accommodating area (364) and the transmission (4 〇) Turn on, in the sleeve s (361) - the side of the side of the elastic beam hole (plus 5), and symmetrically set on both sides of the elastic beam hole (365) - with a perforation (10) clip (36 :) For a screw and nut assembly (368) to lock, so that the clip (367) f elastic beam hole (365) can be locked by the assembly (368) to produce a relative clamping force to promote the casing (361 ) is more stable with the combination of the struts (35) without loosening the M362713, and a struts (352) are provided at the bottom ends of each of the struts (35) against the cover (go), and A flexible element (3631) of nylon thread is arranged to be equiaxed and fixed to each of the pillars (363) so that the strut (35) can be pinched by the strut (352) and the flexible member (3631). For the purpose of reinforcement, without the influence of external force, a plurality of screw holes (301) communicating with the socket tube (32) are longitudinally arranged on the top surface of the cover body (30) for a screw (3〇2) to be locked. The surface of the strut (35), and the strut (35) may also be provided with a through hole (353) opposite to the screw hole (3〇1) and synchronously positioned by the screw (302), and one of the receiving areas (364) One side is convexly convex outward (369) to form a clamping space spring (3691), the transmission device (4G) is provided - the power source of the motor (41) is fixed to the accommodating area (364) and the clamping space (3691), The motor (41) is provided with a smaller control toothed drive wheel (411) and a larger diameter toothed driven wheel (412) to form a reduction gear motor, which is protruded from the center of the driven wheel (412). a connecting rod (42) of an externally threaded section (421) and a centering sleeve (10) is sleeved on the actuating rod (42), so that the actuating rod (42) protrudes from the sleeve hole (431) In addition, at the bottom end of the sleeve hole (431), an internal thread section (432' can be embedded with a nut inside) is locked with the external thread section (421), and the tilt-shield ( 44) and - the nut (44,) is sequentially threaded on the actuating rod (42) and locked on the top surface of the connecting member (43) on both sides of the connecting member (10) [body extension - with a number of perforations ( 433) The set of tabs (434) and each of the mating type and having a plurality of perforations (4 (1) flaps (45, belonging to the inner recessed wings) are locked to form a quadrotor (as shown in the eighth figure), the quadrotor On each of the throwing rods (10) in pairs two-group relative And for different turning rotors of two positive (inverse and two rotors (453). When it wants to fly (as shown in Figure IX), first switch the control switch (221) switch button (22 (1) to (10), so that the control circuit (10) and each drive M362713 device (40) and the power supply (21) are connected. The power supply state is maintained. When the receiver (22) receives the signal transmitted by the remote controller (such as the throttle, the rudder, the elevator and the aileron), the receiver (22) transmits the signal (ie, the amount of current) to the speed control. (25), the speed controller (25) independently drives the motor (41) of each transmission device (40) according to the signal (ie, the amount of current), so that the driving wheel (411) can drive the driven wheel (412), The actuating lever (42), the connecting member (43) and the fin (45) are synchronously rotated 'and the forward rotor (452) and the counter-rotor (453) are controlled by the rotational speed and differential speed of the motor (41). With the ability to fly in the air and make steering, forward or fixed-point rotation in the air, while using the speed controller (25) • the front mixer (24) to control the four-rotor (ie, the rotor 452 and the inverse rotor 453) Steering in the air, and using the sensor when the flying vehicle is flying and turning in the air (23) The function of detecting the angular velocity between the receiver (22) and the mixer (24) balances the differential speed of each motor (41), so that the relative motor (41) is prevented from being excessively differential to maintain the flight. The vehicle is flying in the air and the steering is stable, which reduces the accident rate in the air. In summary, the creation has indeed reached a breakthrough structure, with improved creative content, and at the same time can achieve industrial utilization and progress. • Sexuality and this creation has not been seen in any publication, and it is also novel. When it complies with the provisions of Articles 93 and 94 of the Patent Law, it proposes a new type of patent application according to law. Patent rights, to the pray. Only the above mentioned, only one of the feasible examples of this creation, can not limit the scope of the implementation of this creation; that is, the equivalent changes and modifications made by Dafan according to the scope of patent application for this creation All should still be within the scope of this creation patent. M362713 [Simple description of the diagram] The first picture: is the three-dimensional exploded view of the creation. The second picture: the front of the base of the creation is three-dimensional magnification Fig. 3: A three-dimensional enlarged view of the base of the base of the creation. The fourth picture is a three-dimensional enlarged view of the control circuit and the base of the creation. The fifth picture: the section of the cover of the creation Fig. 6 is a partial enlarged combination diagram of the transmission device of the creation. The seventh picture is the exploded view of the sixth figure. • The eighth picture is the three-dimensional combination of the creation. This is the usage status diagram for this creation. [Main component symbol description] 10.... •• pedestal ll·". "platform 12.... ••first groove section 13....••second groove section 14·· ····通口15.... •• Through hole 16···· •• Limit hole 17···· ••Support foot 20····••Control circuit 2l··..••Power supply 22····••Receiver 221.....·Control switch 2211·•...·Switching key 23····...Inductor 24····••Cluster 25····...Speed controller 26···· •• Fixing seat 261" ...·through hole 30····•• Cover 301- ... screw hole 302... Screw 31-...receiving groove 32.... •• ferrule 33-...top column 331··· ...inner screw hole 34...assembly M362713
35…·_ "撐桿 351". …定位孔 352… …支桿 353... …通孔 36…. ••套接座 361." …套管 362… …套孔 363… …·支柱 3631· •…·撓性元件 364... •…容置區 365." …彈性束孔 366" •…穿孔 367··· …爽片 368" •…組件 369... …撐片 3691· …··夾置空間 40…· ••傳動裝置 4卜·. ..馬達 411... …·主動輪 412- …·被動輪 42…· ••作動桿 421" …·外螺紋段 43…· ••連結件 431- …·套孔 432… •…内螺紋段 433" …·穿孔 434… •…組接片 44···· …墊片 44，· …··螺帽 45···' …翼片 451" …·穿孔 452" 453- •…逆旋翼 A…·. •線路35...·_ "struts 351"....positioning holes 352...struts 353...through holes 36....••sockets 361."...sleeve 362...sleeve 363... Pillar 3631·•··Flexible element 364...•...Receiving area 365."...Elastic beam hole 366" •...Perforation 367····Stable 368" •...Component 369... 3691· ...··Clamping space 40...·••Transmission device 4···················································································· 43...·••Connecting member 431- ...·sleeve hole 432... •...internal thread segment 433" ....perforation 434... •...set tab 44····...shield 44,····nut 45· ··'...Flap 451" ....Perforation 452" 453- •...reverse rotor A...·.
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